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Flow In Serpentine Coolant Passages With Trip Strips
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Author :National Aeronautics and Space Adm Nasa Publisher :Independently Published ISBN 13 :9781792727153 Total Pages :38 pages Book Rating :4.7/5 (271 download)
Book Synopsis Flow in Serpentine Coolant Passages with Trip Strips by : National Aeronautics and Space Adm Nasa
Download or read book Flow in Serpentine Coolant Passages with Trip Strips written by National Aeronautics and Space Adm Nasa and published by Independently Published. This book was released on 2019 with total page 38 pages. Available in PDF, EPUB and Kindle. Book excerpt: Under the subject contract, an effort is being conducted at Scientific Research Associates, Inc. (SRA) to obtain flow field measurements in the coolant passage of a rotating turbine blade with ribbed walls, both in the stationary and rotating frames. The data obtained will be used for validation of computational tools and assessment of turbine blade cooling strategies. The configuration of the turbine blade passage model is given, and the measuring plane locations are given. The model has a four-pass passage with three 180 turns. This geometry was chosen to allow analyses of the velocity measurements corresponding to the heat transfer results obtained by Wagner. Two passes of the passage have a rectangular cross-section of 1.0 in x 0.5 in. Another two passes have a square cross-section of 0.5 in x 0.5 in. Trips with a streamwise pitch to trip height (P/e) = 5 and trip height to coolant passage width (e/Z) = 0.1, were machined along the leading and trailing walls. These dimensions are typical of those used in turbine blade coolant passages. The trips on these walls are staggered by the half-pitch. The trips are skewed at +/- 45 deg, and this allows the effect of trip orientation to be examined. Experiments will be conducted with flow entering the model through the 1.0 in x 0.5 in rectangular passage (Configuration C) and the 0.5 in x 0. 5 in square passage (Configuration D) to examine the effect of passage aspect ratio. Velocity measurements were obtained with a Reynolds number (Re) of 25,000, based on the hydraulic diameter of and bulk mean velocity in the half inch square passage. The coordinate system used in presenting the results for configurations C and D, respectively, is shown. The first, second and third passes of the passage will be referred to as the first, second and third passages, respectively, in later discussion. Streamwise distance (x) from the entrance is normalized by the hydraulic diameter (D). Vertical (y) and tangential (z) distances are normali...
Book Synopsis Flow in Rotating Serpentine Coolant Passages With Skewed Trip Strips by :
Download or read book Flow in Rotating Serpentine Coolant Passages With Skewed Trip Strips written by and published by . This book was released on 1996 with total page 172 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Author :National Aeronautics and Space Administration (NASA) Publisher :Createspace Independent Publishing Platform ISBN 13 :9781723082313 Total Pages :168 pages Book Rating :4.0/5 (823 download)
Book Synopsis Flow in Rotating Serpentine Coolant Passages with Skewed Trip Strips by : National Aeronautics and Space Administration (NASA)
Download or read book Flow in Rotating Serpentine Coolant Passages with Skewed Trip Strips written by National Aeronautics and Space Administration (NASA) and published by Createspace Independent Publishing Platform. This book was released on 2018-07-17 with total page 168 pages. Available in PDF, EPUB and Kindle. Book excerpt: Laser velocimetry was utilized to map the velocity field in serpentine turbine blade cooling passages with skewed trip strips. The measurements were obtained at Reynolds and Rotation numbers of 25,000 and 0.24 to assess the influence of trips, passage curvature and Coriolis force on the flow field. The interaction of the secondary flows induced by skewed trips with the passage rotation produces a swirling vortex and a corner recirculation zone. With trips skewed at +45 deg, the secondary flows remain unaltered as the cross-flow proceeds from the passage to the turn. However, the flow characteristics at these locations differ when trips are skewed at -45 deg. Changes in the flow structure are expected to augment heat transfer, in agreement with the heat transfer measurements of Johnson, et al. The present results show that trips are skewed at -45 deg in the outward flow passage and trips are skewed at +45 deg in the inward flow passage maximize heat transfer. Details of the present measurements were related to the heat transfer measurements of Johnson, et al. to relate fluid flow and heat transfer measurements. Tse, David G.N. and Steuber, Gary Glenn Research Center VELOCITY DISTRIBUTION; TURBINE BLADES; FLOW DISTRIBUTION; CHANNEL FLOW; ROTATING FLUIDS; HEAT TRANSFER; COOLING; FLUID FLOW; SERPENTINE; CURVATURE; VORTICES; SWIRLING; LASER DOPPLER VELOCIMETERS; FLOW MEASUREMENT; CROSS FLOW; FLOW CHARACTERISTICS; CORIOLIS EFFECT...
Book Synopsis 1996 Coolant Flow Management Workshop by :
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Book Synopsis Flow in a Rotating Square Serpentine Coolant Passage with Skewed Trips by : David G. N. Tse
Download or read book Flow in a Rotating Square Serpentine Coolant Passage with Skewed Trips written by David G. N. Tse and published by . This book was released on 1997 with total page 0 pages. Available in PDF, EPUB and Kindle. Book excerpt: Presented at the International Gas Turbine & Aeroegine Congress & Exhibition, Orlando, FL, Jun 2-Jun 5, 1997.
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Book Synopsis Effects of Rotation on Coolant Passage Heat Transfer. Volume 2: Coolant Passages with Trips Normal and Skewed to the Flow by :
Download or read book Effects of Rotation on Coolant Passage Heat Transfer. Volume 2: Coolant Passages with Trips Normal and Skewed to the Flow written by and published by . This book was released on 1993 with total page 132 pages. Available in PDF, EPUB and Kindle. Book excerpt:
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Book Synopsis Heat Transfer in Rotating Serpentine Passages with Selected Model Orientation for Smooth Or Skewed Trip Walls by :
Download or read book Heat Transfer in Rotating Serpentine Passages with Selected Model Orientation for Smooth Or Skewed Trip Walls written by and published by . This book was released on 1993 with total page 14 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Thermal Engineering in Power Systems by : Ryoichi Amano
Download or read book Thermal Engineering in Power Systems written by Ryoichi Amano and published by WIT Press. This book was released on 2008 with total page 417 pages. Available in PDF, EPUB and Kindle. Book excerpt: Research and development in thermal engineering for power systems are of significant importance to many scientists who are engaged in research and design work in power-related industries and laboratories. This book focuses on variety of research areas including Components of Compressor and Turbines that are used for both electric power systems and aero engines, Fuel Cells, Energy Conversion, and Energy Reuse and Recycling Systems. To be competitive in today's market, power systems need to reduce the operating costs, increase capacity factors and deal with many other tough issues. Heat Transfer and fluid flow issues are of great significance and it is likely that a state-of-the-art edited book with reference to power systems will make a contribution for design and R&D engineers and the development towards sustainable energy systems.
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